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VKS-D
Part of VKS series
Russian winged orbital launch vehicle. Air launched from An-225. Release conditions: Piggy-back, 275,000 kg, 38.0 m length x 24.0 m wingspan, 900 kph at 9,500 m altitude. Effective velocity gain compared to vertical launch 270 m/s.

Status: Study 1988. Payload: 6,000 kg (13,200 lb). Gross mass: 275,000 kg (606,000 lb). Apogee: 200 km (120 mi).

LEO Payload: 6,000 kg (13,200 lb) to a 200 km orbit at 51.00 degrees.

Family: aircraft-launched, orbital launch vehicle, Winged. Country: Russia. Agency: Molniya bureau.
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